US20140286632A1 - Focal plane shutter and optical device - Google Patents
Focal plane shutter and optical device Download PDFInfo
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- US20140286632A1 US20140286632A1 US14/175,280 US201414175280A US2014286632A1 US 20140286632 A1 US20140286632 A1 US 20140286632A1 US 201414175280 A US201414175280 A US 201414175280A US 2014286632 A1 US2014286632 A1 US 2014286632A1
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- iron core
- iron
- plating
- iron piece
- drive lever
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- 230000003287 optical effect Effects 0.000 title claims description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 320
- 229910052742 iron Inorganic materials 0.000 claims abstract description 112
- 238000007747 plating Methods 0.000 claims abstract description 51
- 238000000034 method Methods 0.000 claims abstract description 7
- 230000008569 process Effects 0.000 claims abstract description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 4
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- 238000001179 sorption measurement Methods 0.000 description 26
- 230000000052 comparative effect Effects 0.000 description 8
- 230000008859 change Effects 0.000 description 6
- 230000009467 reduction Effects 0.000 description 6
- 238000005299 abrasion Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 230000004907 flux Effects 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Classifications
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B9/00—Exposure-making shutters; Diaphragms
- G03B9/08—Shutters
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B9/00—Exposure-making shutters; Diaphragms
- G03B9/08—Shutters
- G03B9/36—Sliding rigid plate
Definitions
- the present invention relates to focal plane shutters and optical device.
- a focal plane shutter is equipped with: an iron core of an electromagnet; and a drive lever holding an iron piece, the magnetic attraction force being generated between the iron piece and the electromagnet.
- the drive lever drives blades.
- the drive lever is biased by a biasing member such that the iron piece is moved away from the iron core of the electromagnet.
- the electromagnet is energized in a state where the iron piece abuts the iron core, so that the magnetic attraction force is generated between the iron piece and the iron core.
- the iron piece is adsorbed to and held by the iron core against the biasing force of the biasing member.
- the iron piece of the drive lever repeatedly abuts the iron core of the electromagnet, so that the adsorption force of the iron piece to the iron core might decrease. This is conceivably because the repeated abutment of the iron piece with the iron core might cause abrasion of the adsorption surface of the iron piece, so that the adsorption surface might be made uneven or the adsorption surface might be attached with abrasion powder.
- the adsorption force of the iron piece to the iron core decreases in this way. This shortens the period from the time when the energization of the electromagnet is stopped to the time when the iron piece is moved away from the iron core by making the adsorption force lower than the biasing force of the biasing member.
- the speed of the blades also changes to increase the error between the actual exposure period and the desired exposure period assumed beforehand.
- the image quality might be influenced.
- a focal plane shutter including: a board including an opening; a blade opening or closing the opening; an electromagnet including an iron core and a coil for energizing the iron core; and a drive lever holding an iron piece capable of being adsorbed to the iron core, capable of moving such that iron piece is moved into and away from the iron core, and driving the blade, wherein a plating process is performed on the iron core and the iron piece, a Vickers hardness of a plating of the iron piece is greater than that of a plating of the iron core, and a difference in the Vickers hardness between the plating of the iron piece and the plating of the iron core is 100 HV or more.
- FIG. 1 is a front view of a focal plane shutter according to the present embodiment
- FIG. 2 is an explanatory view of an operation of the focal plane shutter
- FIG. 3 is an explanatory view of the operation of the focal plane shutter
- FIG. 4 is a perspective view of a trailing blade-drive lever
- FIG. 5 is an explanatory view of an operation of the trailing blade-drive lever
- FIG. 6 is an explanatory view of the operation of the trailing blade-drive lever
- FIG. 7A is a graph of a change in voltage which was applied to an electromagnet and which was needed for generating a constant adsorption force between an iron piece and an iron core before and after an endurance test of the focal plane shutter according to the present embodiment
- FIG. 7B is a graph of a change in voltage which was applied to an electromagnet and which was needed for generating a constant adsorption force between an iron piece and an iron core before and after an endurance test of a focal plane shutter according to the comparative example.
- FIG. 1 is a front view of a focal plane shutter according to the present embodiment.
- a focal plane shutter 1 includes: a board 10 ; blades 21 a to 24 a and 21 b to 24 b; drive arms 31 a, 32 a, 31 b, and 32 b; and electromagnets 70 A and 70 B.
- the board 10 is made of a synthetic resin, and includes an opening 11 with a rectangular shape.
- Each of the blades 21 a to 24 a and 21 b to 24 b is made of a synthetic resin and is thinly formed.
- each of the drive arms 31 a, 32 a, 31 b , and 32 b is made of a metal sheet to retain its strength.
- Each of the blades 21 a to 24 a and 21 b to 24 b move between a position of receding from the opening 11 and a position of covering at least part of the opening 11 .
- FIG. 1 illustrates the leading blades 20 A in an overlapped state and the trailing blades 20 B in an expanded state. In FIG. 1 , the leading blades 20 A recedes from the opening 11 and the trailing blades 20 B close the opening 11 .
- the leading blades 20 A are connected to the drive arms 31 a and 32 a.
- the trailing blades 20 B are connected to the drive arms 31 b and 32 b.
- These drive arms 31 a, 32 a, 31 b, and 32 b are swingably supported by the board 10 .
- a leading blade-drive lever 40 A and a trailing blade-drive lever 40 B for respectively driving the drive arms 31 a and 32 b are provided in the board 10 .
- the leading blade-drive lever 40 A and the trailing blade-drive lever 40 B are supported by the board 10 to be swingable in a predetermined range. Specifically, the leading blade-drive lever 40 A is supported to swing about a spindle provided in the board 10 .
- the swinging range of the leading blade-drive lever 40 A is limited by a rubber, mentioned later, provided at an end portion of a slot formed in the board 10 . This is applied to the trailing blade-drive lever 40 B.
- the drive arm 31 a is connected to the leading blade-drive lever 40 A.
- the drive arm 32 b is connected to the trailing blade-drive lever 40 B.
- the swinging of the leading blade-drive lever 40 A causes the drive arm 31 a to swing, thereby moving the leading blades 20 A.
- the swinging of the trailing blade-drive lever 40 B causes the drive arm 32 b to swing, thereby moving the trailing blades 20 B.
- the leading blade-drive lever 40 A and the trailing blade-drive lever 40 B each holds an iron piece which does not have a reference numeral.
- the leading blade-drive lever 40 A can swing between the position where the iron piece abuts the electromagnet 70 A and the position where the iron piece recedes from the electromagnet 70 A. This is applied to the trailing blade-drive lever 40 B.
- leading blade-drive lever 40 A is biased by a spring, not illustrated, in such a direction as to move away from the electromagnet 70 A.
- trailing blade-drive lever 40 B is biased by a spring, not illustrated, in such a direction as to move away from the electromagnet 70 B.
- Ratchet wheels 50 A and 50 B engage the leading blade-drive lever 40 A and the trailing blade-drive lever 40 B, respectively, through the springs mentioned above.
- One end of the spring which biases the leading blade-drive lever 40 A in such a direction as to move away from the electromagnet 70 A, engages the ratchet wheel 50 A.
- the other end of the spring engages the leading blade-drive lever 40 A.
- the biasing force of the spring is adjusted by adjusting the rotational amount of the ratchet wheel 50 A beforehand in assembling the focal plane shutter 1 .
- the ratchet wheel 50 B also has a function similar to that of the ratchet wheel 50 A.
- the leading blades 20 A and the trailing blades 20 B of the focal plane shutter 1 are driven at the speed corresponding to the biasing force of the spring. For example, the leading blades 20 A are driven faster as the rotational amount of the ratchet wheel 50 A is larger. This configuration also is applicable to the trailing blades 20 B.
- the biasing force of the spring is set in assembling. After that, the leading blades 20 A and the trailing blades 20 B are always driven at a predetermined speed based on the set biasing force.
- the electromagnet 70 A is energized, thereby adsorbing the iron piece of the leading blade-drive lever 40 A.
- the electromagnet 70 B is energized, thereby adsorbing the iron piece of the trailing blade-drive lever 40 B.
- FIGS. 1 to 3 are explanatory views of the operation of the focal plane shutter 1 .
- FIG. 2 illustrates the focal plane shutter 1 in an initial state.
- a set lever not illustrated is secured to an initial position
- the leading blades 20 A are expanded to close the opening 11
- the trailing blades 20 B are overlapped each other to recede from the opening 11 .
- the iron pieces of the leading blade-drive lever 40 A and the trailing blade-drive lever 40 B abut the electromagnets 70 A and 70 B respectively by the set lever, and are set in such an initial position as to be adsorbed to them respectively.
- a release button of the camera is pushed to energize coils of the electromagnets 70 A and 70 B, whereby the iron piece of the leading blade-drive lever 40 A is adsorbed to the electromagnet 70 A and the iron piece of the trailing blade-drive lever 40 B is adsorbed to the electromagnet 70 B.
- the set lever moves away from the leading blade-drive lever 40 A and the trailing blade-drive lever 40 B.
- the leading blade-drive lever 40 A and the trailing blade-drive lever 40 B remain adsorbed to the electromagnets 70 A and 70 B, respectively.
- the energization of the coil of the electromagnet 70 A is stopped, thereby rotating the leading blade-drive lever 40 A in a clockwise direction by the biasing force of the spring as illustrated in FIG. 3 . Therefore, the leading blades 20 A move away from the opening 11 to be in the overlapped state. Also, the energization of the coil of the electromagnet 70 B maintains for a predetermined period based on the exposure period, whereas the trailing blades 20 B remain away from the opening 11 .
- FIG. 3 illustrates an exposed state.
- FIG. 1 illustrates the state just after the exposure operation is finished. In such a way, one cycle of shooting is finished.
- leading blade-drive lever 40 A and the trailing blade-drive lever 40 B are rotated counterclockwise by the set lever not illustrated. Therefore, the leading blades 20 A are expanded to close the opening 11 and the trailing blades 20 B are overlapped each other to recede from the opening 11 , whereby the state is returned to the initial state illustrated in FIG. 2 .
- FIG. 4 is a perspective view of the trailing blade-drive lever 40 B. Firstly, an outline of the trailing blade-drive lever 40 B will be described. Additionally, the structure is partially omitted in FIG. 4 .
- the trailing blade-drive lever 40 B includes: a base portion 41 b with a board shape; a cylindrical portion 41 b 1 standing on the base portion 41 b; a roller portion 41 b 2 ; and a drive pin 41 b 8 .
- the ratchet wheel 50 B and a spring biasing the trailing blade-drive lever 40 B are arranged around the cylindrical portion 41 b 1 .
- a spindle provided on the board 10 is fitted into the cylindrical portion 41 b 1 .
- the trailing blade-drive lever 40 B rotates a predetermined range about the spindle fitted into the cylindrical portion 41 b 1 .
- the roller portion 41 b 2 is pushed by a set lever not illustrated.
- the roller portion 41 b 2 is pushed by the set lever to rotate the trailing blade-drive lever 40 B about the cylindrical portion 41 b 1 .
- the drive pin 41 b 8 extends downwardly from the base portion 41 b.
- the drive pin 41 b 8 is fitted into a hole formed in the drive arm 32 b.
- a support portion 42 b is provided on the base portion 41 b.
- the support portion 42 b is provided for supporting an iron piece 46 b.
- the iron piece 46 b is adsorbed to the electromagnet 70 B.
- the iron piece 46 b is coupled to a spindle portion 45 b.
- the spindle portion 45 b is made of a metal.
- the iron piece 46 b is formed into a rectangular shape with a given thickness.
- the support portion 42 b includes: guide portions 43 b and 44 b along the side of the iron piece 46 b.
- the guide portions 43 b and 44 b restricts the iron piece 46 b from rotating about the spindle portion 45 b.
- a second biasing member 49 b is inserted between the guide portion 43 b and a side surface of the iron piece 46 b.
- the second biasing member 49 b is an elastically deformable spring with a plate shape.
- the second biasing member 49 b includes: a base portion 49 b 1 extending linearly along the side surface of the iron piece 46 b; and an engagement portion 49 b 2 continuous with the upper end of the base portion 49 b 1 and having an L shape when viewed from its side.
- the engagement portion 49 b 2 engages the support portion 42 b and is held thereby.
- the second biasing member 49 b is provided for biasing the iron piece 46 b in a given direction and is provided for abutting the iron piece 46 b with an iron core 73 b in a stable posture.
- FIGS. 5 and 6 are explanatory viewed of the operation of the trailing blade-drive lever 40 B.
- the structure of the trailing blade-drive lever 40 B is partially omitted in FIGS. 5 and 6 .
- FIG. 5 illustrates a state where the trailing blade-drive lever 40 B is spaced apart from the electromagnet 70 B.
- FIG. 6 illustrates a state where the iron piece 46 b of the trailing blade-drive lever 40 B is adsorbed to the electromagnet 70 B.
- the opening 11 is located in the right side of the trailing blade-drive lever 40 B in FIGS. 5 and 6 .
- the board 10 is formed with an arc-shaped slot 13 b for escaping the movement of the drive pin 41 b 8 .
- the slot 13 b is provided at its one end portion with a rubber 13 b 1 for preventing the drive pin 41 b 8 from bounding.
- the electromagnet 70 B includes: the iron core 73 b; a coil 79 b for exciting the iron core 73 b; and a bobbin 78 b around which the coil 79 b is wound. The energization of the coil 79 b generates the magnetic attraction force in the iron core 73 b.
- the trailing blade-drive lever 40 B is rotated about the cylindrical portion 41 b 1 counterclockwise by the set lever from a state illustrated in FIG. 5 . Therefore, the drive pin 41 b 8 moves within the slot 13 b and then the iron piece 46 b abuts the iron core 73 b . Afterward, the coil 79 b is energized, and then the iron piece 46 b is adsorbed to the iron core 73 b. As long as the coil 79 b is energized even after the set lever recedes, the iron piece 46 b is continuously adsorbed to the iron core 73 b.
- the iron piece 46 b engages the spindle portion 45 b and is capable of reciprocating axially with respect thereto.
- a first biasing member 47 b is provided between the support portion 42 b and the iron piece 46 b.
- the first biasing member 47 b is a spring with a coil shape.
- the spindle portion 45 b is inserted into the first biasing member 47 b.
- the first biasing member 47 b biases the iron piece 46 b toward the axial direction of the spindle portion 45 b, that is, toward the electromagnet 70 B.
- the iron piece 46 b and the iron core 73 b are made of pure iron (SUY), and plating thereof ensure a desired hardness by having heated the pure iron after performing an electroless nickel plating process on the pure iron.
- the base material of the iron piece 46 b and the iron core 73 b may be any soft magnetic material other than the pure iron.
- a Vickers hardness of the plating of the iron piece 46 b is greater than that of the plating of the iron core 73 b.
- the Vickers hardness of the plating of the iron piece 46 b is 950 HV plus or minus 50 HV.
- the Vickers hardness of the plating of the iron core 73 b is 750 HV plus or minus 50 HV.
- the difference in the Vickers hardness between the plating of the iron piece 46 b and the plating of the iron core 73 b is 100 HV or more and 300 HV or less.
- the Vickers hardness of the plating of the iron piece 46 b is 900 HV or more and 1000 HV or less.
- the Vickers hardness of the plating of the iron core 73 b is 700 HV or more and 800 HV or less. Additionally, the same configuration is applicable to the iron piece of the leading blade-drive lever 40 A and the iron core of the electromagnet 70 A.
- a change in the adsorption force between the iron piece 46 b and the iron core 73 b was verified before and after an endurance test of the focal plane shutter 1 according to the present embodiment. Specifically, the voltage which was applied to the coil 79 b and which was needed for generating a constant adsorption force between the iron piece 46 b and the iron core 73 b was measured before and after the endurance test of the focal plane shutter 1 according to the present embodiment. In the endurance test, the trailing blade-drive lever 40 B reciprocated several times such that the iron piece 46 b abutted the iron core 73 b several times. FIG.
- FIG. 7A is a graph of the change in the voltage which was applied to the electromagnet 70 B and which was needed for generating a constant adsorption force between the iron piece 46 b and the iron core 73 b before and after the endurance test of the focal plane shutter 1 according to the present embodiment.
- the change of the voltage applied to the electromagnet 70 B was verified by use of three samples under the same condition before and after the endurance test.
- the voltage which was applied to the coil 79 b and which was needed for generating a constant adsorption force between the iron piece 46 b and the iron core 73 b was not greatly changed before and after the endurance test. This means that the adsorption force between the iron piece 46 b and the iron core 73 b was not greatly changed even in a case where a constant voltage was applied to the electromagnet 70 B before and after the endurance test.
- FIG. 7B is a graph of a change in the voltage which was applied to the electromagnet and which was needed for generating a constant adsorption force between the iron piece and the iron core before and after the endurance test of the focal plane shutter according to the comparative example.
- the voltage which was applied to the electromagnet and which was needed for generating a constant adsorption force after the endurance test was higher than that before the endurance test.
- the adsorption force generated between the iron piece and the iron core after the endurance test was lower than that before the endurance test.
- the reason is considered as follows.
- the iron piece and the iron core in the comparative example are the same in the Vickers hardness, and the Vickers hardness of the iron piece in the comparative example is smaller than that of the iron piece 46 b in the present embodiment.
- the iron piece in the comparative example is easy to be worn down.
- the adsorption surface of the iron piece is attached with abrasion powder or is deformed to be uneven.
- an air gap is formed between the iron piece and the iron core, and the area of the absorption is reduced. Therefore, supposedly, a reduction in the spatial magnetic flux density or a reduction in the surface magnetic flux density causes a reduction in the adsorption surface.
- the voltage with the same value is applied to the electromagnet in a camera.
- the long-term use of a camera with the focal plane shutter according to the comparative example causes a reduction in the adsorption force.
- This causes a reduction in the period from the time when the energization of the electromagnet is stopped to the time when the iron piece is moved away from the iron core by the biasing force of the biasing member.
- the timing when the blades start moving might be advanced to influence the exposure period.
- the adsorption force is not greatly changed before and after the endurance test. This is conceivably because it becomes difficult to wear down the iron piece 46 b due to the Vickers hardness of the plating of the iron piece 46 b which is greater than that of the plating of the iron core 73 b. Accordingly, in the focal plane shutter 1 according to the present embodiment, a reduction in the adsorption force is suppressed even for long-term use. Therefore, even when the focal plane shutter 1 is used for a long time, the constant exposure period can be maintained, thereby suppressing the error of the exposure period from increasing.
- the difference in the Vickers hardness between the plating of the iron piece 46 b and the plating of the iron core 73 b is 100 HV or more.
- the difference in the Vickers hardness between the plating of the iron piece 46 b and the plating of the iron core 73 b should be 300 HV or less.
- the Vickers hardness of the plating of the iron piece 46 b should be 900 HV or more and 1000 HV or less. It is preferable that the Vickers hardness of the plating of the iron core 73 b should be 700 HV or more and 800 HV or less.
- the present invention may be applied to a self-holding electromagnet.
- a self-holding electromagnet a permanent magnet which gives magnetic force to an iron core is fixed thereto, and the iron core can adsorb and hold an iron piece in a non-energization state.
- the enegization of a coil wound around the iron core generates a magnetic field around the coil so as to reduce the magnetic force of the permanent magnet.
- the focal plane shutter according to the present embodiment can be employed in an optical device such as a still camera or a digital camera.
- a focal plane shutter including: a board including an opening; a blade opening or closing the opening; an electromagnet including an iron core and a coil for energizing the iron core; and a drive lever holding an iron piece capable of being adsorbed to the iron core, capable of moving such that iron piece is moved into and away from the iron core, and driving the blade, wherein a plating process is performed on the iron core and the iron piece, a Vickers hardness of a plating of the iron piece is greater than that of a plating of the iron core, and a difference in the Vickers hardness between the plating of the iron piece and the plating of the iron core is 100 HV or more.
- an optical device including the above focal plane shutter.
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Abstract
Description
- This application is based upon and claims the benefit of priority of the prior Japanese Patent Application No. 2013-060209, filed on Mar. 22, 2013, the entire contents of which are incorporated herein by reference.
- (i) Technical Field
- The present invention relates to focal plane shutters and optical device.
- (ii) Related Art
- A focal plane shutter is equipped with: an iron core of an electromagnet; and a drive lever holding an iron piece, the magnetic attraction force being generated between the iron piece and the electromagnet. The drive lever drives blades. The drive lever is biased by a biasing member such that the iron piece is moved away from the iron core of the electromagnet. The electromagnet is energized in a state where the iron piece abuts the iron core, so that the magnetic attraction force is generated between the iron piece and the iron core. Thus, the iron piece is adsorbed to and held by the iron core against the biasing force of the biasing member. The energization of the electromagnet is stopped in the state where the iron piece is adsorbed to the iron core, so that the adsorption force of the iron piece to the iron core is lower than the biasing force of the biasing member. Thus, the drive lever moves in accordance with the biasing force of the biasing member such that the iron piece is moved away from the iron core. In this way, the drive lever drives the blades by use of the magnetic attraction force of the electromagnet and the biasing force of the biasing member. Japanese Unexamined Patent Application Publication No. 2004-029277 discloses such a focal plane shutter.
- The iron piece of the drive lever repeatedly abuts the iron core of the electromagnet, so that the adsorption force of the iron piece to the iron core might decrease. This is conceivably because the repeated abutment of the iron piece with the iron core might cause abrasion of the adsorption surface of the iron piece, so that the adsorption surface might be made uneven or the adsorption surface might be attached with abrasion powder.
- The adsorption force of the iron piece to the iron core decreases in this way. This shortens the period from the time when the energization of the electromagnet is stopped to the time when the iron piece is moved away from the iron core by making the adsorption force lower than the biasing force of the biasing member. Thus, the speed of the blades also changes to increase the error between the actual exposure period and the desired exposure period assumed beforehand. Thus, the image quality might be influenced.
- Further, the same problem might occur in a self-holding electromagnet in which a magnet is secured to an iron core, an iron piece can be adsorbed to the iron core in a non-energized state, and the adsorption force can be reduced by energization.
- It is therefore an object of the present invention to provide a focal plane shutter and an optical device that suppress an error of an exposure period from increasing.
- According to an aspect of the present invention, there is provided a focal plane shutter including: a board including an opening; a blade opening or closing the opening; an electromagnet including an iron core and a coil for energizing the iron core; and a drive lever holding an iron piece capable of being adsorbed to the iron core, capable of moving such that iron piece is moved into and away from the iron core, and driving the blade, wherein a plating process is performed on the iron core and the iron piece, a Vickers hardness of a plating of the iron piece is greater than that of a plating of the iron core, and a difference in the Vickers hardness between the plating of the iron piece and the plating of the iron core is 100 HV or more.
-
FIG. 1 is a front view of a focal plane shutter according to the present embodiment; -
FIG. 2 is an explanatory view of an operation of the focal plane shutter; -
FIG. 3 is an explanatory view of the operation of the focal plane shutter; -
FIG. 4 is a perspective view of a trailing blade-drive lever; -
FIG. 5 is an explanatory view of an operation of the trailing blade-drive lever; -
FIG. 6 is an explanatory view of the operation of the trailing blade-drive lever; -
FIG. 7A is a graph of a change in voltage which was applied to an electromagnet and which was needed for generating a constant adsorption force between an iron piece and an iron core before and after an endurance test of the focal plane shutter according to the present embodiment, andFIG. 7B is a graph of a change in voltage which was applied to an electromagnet and which was needed for generating a constant adsorption force between an iron piece and an iron core before and after an endurance test of a focal plane shutter according to the comparative example. - An embodiment will be described with reference to the drawings as follows. In the present embodiment, a focal plane shutter will be described as an example of a blade drive device.
FIG. 1 is a front view of a focal plane shutter according to the present embodiment. As illustrated inFIG. 1 , afocal plane shutter 1 includes: aboard 10;blades 21 a to 24 a and 21 b to 24 b; drive 31 a, 32 a, 31 b, and 32 b; andarms 70A and 70B. Theelectromagnets board 10 is made of a synthetic resin, and includes an opening 11 with a rectangular shape. Each of theblades 21 a to 24 a and 21 b to 24 b is made of a synthetic resin and is thinly formed. Also, each of the 31 a, 32 a, 31 b, and 32 b is made of a metal sheet to retain its strength. Each of thedrive arms blades 21 a to 24 a and 21 b to 24 b move between a position of receding from the opening 11 and a position of covering at least part of the opening 11. - Four
blades 21 a to 24 a configure leadingblades 20A. Fourblades 21 b to 24 b configuretrailing blades 20B.FIG. 1 illustrates the leadingblades 20A in an overlapped state and thetrailing blades 20B in an expanded state. InFIG. 1 , the leadingblades 20A recedes from the opening 11 and thetrailing blades 20B close theopening 11. - The leading
blades 20A are connected to the 31 a and 32 a. Thedrive arms trailing blades 20B are connected to the 31 b and 32 b. These drivedrive arms 31 a, 32 a, 31 b, and 32 b are swingably supported by thearms board 10. - A leading blade-
drive lever 40A and a trailing blade-drive lever 40B for respectively driving the 31 a and 32 b are provided in thedrive arms board 10. The leading blade-drive lever 40A and the trailing blade-drive lever 40B are supported by theboard 10 to be swingable in a predetermined range. Specifically, the leading blade-drive lever 40A is supported to swing about a spindle provided in theboard 10. The swinging range of the leading blade-drive lever 40A is limited by a rubber, mentioned later, provided at an end portion of a slot formed in theboard 10. This is applied to the trailing blade-drive lever 40B. - The
drive arm 31 a is connected to the leading blade-drive lever 40A. Thedrive arm 32 b is connected to the trailing blade-drive lever 40B. The swinging of the leading blade-drive lever 40A causes thedrive arm 31 a to swing, thereby moving the leadingblades 20A. Likewise, the swinging of the trailing blade-drive lever 40B causes thedrive arm 32 b to swing, thereby moving thetrailing blades 20B. - The leading blade-
drive lever 40A and the trailing blade-drive lever 40B each holds an iron piece which does not have a reference numeral. The leading blade-drive lever 40A can swing between the position where the iron piece abuts theelectromagnet 70A and the position where the iron piece recedes from theelectromagnet 70A. This is applied to the trailing blade-drive lever 40B. - Also, the leading blade-
drive lever 40A is biased by a spring, not illustrated, in such a direction as to move away from theelectromagnet 70A. Likewise, the trailing blade-drive lever 40B is biased by a spring, not illustrated, in such a direction as to move away from theelectromagnet 70B. -
50A and 50B engage the leading blade-Ratchet wheels drive lever 40A and the trailing blade-drive lever 40B, respectively, through the springs mentioned above. One end of the spring, which biases the leading blade-drive lever 40A in such a direction as to move away from theelectromagnet 70A, engages theratchet wheel 50A. The other end of the spring engages the leading blade-drive lever 40A. The biasing force of the spring is adjusted by adjusting the rotational amount of theratchet wheel 50A beforehand in assembling thefocal plane shutter 1. Theratchet wheel 50B also has a function similar to that of theratchet wheel 50A. The leadingblades 20A and the trailingblades 20B of thefocal plane shutter 1 are driven at the speed corresponding to the biasing force of the spring. For example, the leadingblades 20A are driven faster as the rotational amount of theratchet wheel 50A is larger. This configuration also is applicable to the trailingblades 20B. In thefocal plane shutter 1 according to the present embodiment, the biasing force of the spring is set in assembling. After that, the leadingblades 20A and the trailingblades 20B are always driven at a predetermined speed based on the set biasing force. - The
electromagnet 70A is energized, thereby adsorbing the iron piece of the leading blade-drive lever 40A. Likewise, theelectromagnet 70B is energized, thereby adsorbing the iron piece of the trailing blade-drive lever 40B. - Next, the operation of the
focal plane shutter 1 will be described.FIGS. 1 to 3 are explanatory views of the operation of thefocal plane shutter 1. Here,FIG. 2 illustrates thefocal plane shutter 1 in an initial state. In this initial state, a set lever not illustrated is secured to an initial position, the leadingblades 20A are expanded to close theopening 11, and the trailingblades 20B are overlapped each other to recede from theopening 11. In this initial state, the iron pieces of the leading blade-drive lever 40A and the trailing blade-drive lever 40B abut the 70A and 70B respectively by the set lever, and are set in such an initial position as to be adsorbed to them respectively.electromagnets - In shooting, a release button of the camera is pushed to energize coils of the
70A and 70B, whereby the iron piece of the leading blade-electromagnets drive lever 40A is adsorbed to theelectromagnet 70A and the iron piece of the trailing blade-drive lever 40B is adsorbed to theelectromagnet 70B. After that, the set lever moves away from the leading blade-drive lever 40A and the trailing blade-drive lever 40B. At this time, the leading blade-drive lever 40A and the trailing blade-drive lever 40B remain adsorbed to the 70A and 70B, respectively.electromagnets - Afterward, the energization of the coil of the
electromagnet 70A is stopped, thereby rotating the leading blade-drive lever 40A in a clockwise direction by the biasing force of the spring as illustrated inFIG. 3 . Therefore, the leadingblades 20A move away from theopening 11 to be in the overlapped state. Also, the energization of the coil of theelectromagnet 70B maintains for a predetermined period based on the exposure period, whereas the trailingblades 20B remain away from theopening 11. - This causes the
opening 11 to be in an opened state.FIG. 3 illustrates an exposed state. - After a predetermined period lapses from a time when the release button is pushed, the energization of the coil of the
electromagnet 70B is stopped, and then the trailing blade-drive lever 40B rotates clockwise by the biasing force of the spring. Therefore, the trailingblades 20B are expanded to close theopening 11. The trailing blade-drive lever 40B abuts a rubber, as will be mentioned later, for preventing bound, provided at an end of the slot formed in theboard 10.FIG. 1 illustrates the state just after the exposure operation is finished. In such a way, one cycle of shooting is finished. - Next, the leading blade-
drive lever 40A and the trailing blade-drive lever 40B are rotated counterclockwise by the set lever not illustrated. Therefore, the leadingblades 20A are expanded to close theopening 11 and the trailingblades 20B are overlapped each other to recede from theopening 11, whereby the state is returned to the initial state illustrated inFIG. 2 . - Next, the drive lever will be described. Although the leading blade-
drive lever 40A and the trailing blade-drive lever 40B differ in shape from each other, they substantially have the same configuration and the same parts. The following description will be given of only the trailing blade-drive lever 40B.FIG. 4 is a perspective view of the trailing blade-drive lever 40B. Firstly, an outline of the trailing blade-drive lever 40B will be described. Additionally, the structure is partially omitted inFIG. 4 . - The trailing blade-
drive lever 40B includes: abase portion 41 b with a board shape; acylindrical portion 41b 1 standing on thebase portion 41 b; aroller portion 41 b 2; and adrive pin 41 b 8. Theratchet wheel 50B and a spring biasing the trailing blade-drive lever 40B are arranged around thecylindrical portion 41b 1. Also, a spindle provided on theboard 10 is fitted into thecylindrical portion 41b 1. The trailing blade-drive lever 40B rotates a predetermined range about the spindle fitted into thecylindrical portion 41b 1. - The
roller portion 41 b 2 is pushed by a set lever not illustrated. Theroller portion 41 b 2 is pushed by the set lever to rotate the trailing blade-drive lever 40B about thecylindrical portion 41b 1. Thedrive pin 41 b 8 extends downwardly from thebase portion 41 b. Thedrive pin 41 b 8 is fitted into a hole formed in thedrive arm 32 b. - A
support portion 42 b is provided on thebase portion 41 b. Thesupport portion 42 b is provided for supporting aniron piece 46 b. Theiron piece 46 b is adsorbed to theelectromagnet 70B. Theiron piece 46 b is coupled to aspindle portion 45 b. Thespindle portion 45 b is made of a metal. Theiron piece 46 b is formed into a rectangular shape with a given thickness. Thesupport portion 42 b includes: guide 43 b and 44 b along the side of theportions iron piece 46 b. The 43 b and 44 b restricts theguide portions iron piece 46 b from rotating about thespindle portion 45 b. - A
second biasing member 49 b is inserted between theguide portion 43 b and a side surface of theiron piece 46 b. Thesecond biasing member 49 b is an elastically deformable spring with a plate shape. Thesecond biasing member 49 b includes: abase portion 49b 1 extending linearly along the side surface of theiron piece 46 b; and anengagement portion 49 b 2 continuous with the upper end of thebase portion 49 b 1 and having an L shape when viewed from its side. Theengagement portion 49 b 2 engages thesupport portion 42 b and is held thereby. Thesecond biasing member 49 b is provided for biasing theiron piece 46 b in a given direction and is provided for abutting theiron piece 46 b with aniron core 73 b in a stable posture. - Next, an operation of the trailing blade-
drive lever 40B will be described.FIGS. 5 and 6 are explanatory viewed of the operation of the trailing blade-drive lever 40B. The structure of the trailing blade-drive lever 40B is partially omitted inFIGS. 5 and 6 .FIG. 5 illustrates a state where the trailing blade-drive lever 40B is spaced apart from theelectromagnet 70B.FIG. 6 illustrates a state where theiron piece 46 b of the trailing blade-drive lever 40B is adsorbed to theelectromagnet 70B. Theopening 11 is located in the right side of the trailing blade-drive lever 40B inFIGS. 5 and 6 . - The
board 10 is formed with an arc-shapedslot 13 b for escaping the movement of thedrive pin 41 b 8. Also, theslot 13 b is provided at its one end portion with arubber 13b 1 for preventing thedrive pin 41 b 8 from bounding. Theelectromagnet 70B includes: theiron core 73 b; acoil 79 b for exciting theiron core 73 b; and abobbin 78 b around which thecoil 79 b is wound. The energization of thecoil 79 b generates the magnetic attraction force in theiron core 73 b. - The trailing blade-
drive lever 40B is rotated about thecylindrical portion 41b 1 counterclockwise by the set lever from a state illustrated inFIG. 5 . Therefore, thedrive pin 41 b 8 moves within theslot 13 b and then theiron piece 46 b abuts theiron core 73 b. Afterward, thecoil 79 b is energized, and then theiron piece 46 b is adsorbed to theiron core 73 b. As long as thecoil 79 b is energized even after the set lever recedes, theiron piece 46 b is continuously adsorbed to theiron core 73 b. When the energization of thecoil 79 b is stopped, the magnetic attraction force generated between theiron piece 46 b and theiron core 73 b disappears, and then the trailing-blade drive lever 40B is rotated clockwise by the biasing force of the spring not illustrated. The trailing blade-drive lever 40B is operated in such a way. - Additionally, the
iron piece 46 b engages thespindle portion 45 b and is capable of reciprocating axially with respect thereto. A first biasingmember 47 b is provided between thesupport portion 42 b and theiron piece 46 b. Thefirst biasing member 47 b is a spring with a coil shape. Thespindle portion 45 b is inserted into the first biasingmember 47 b. Thefirst biasing member 47 b biases theiron piece 46 b toward the axial direction of thespindle portion 45 b, that is, toward theelectromagnet 70B. - Herein, in the present embodiment, the
iron piece 46 b and theiron core 73 b are made of pure iron (SUY), and plating thereof ensure a desired hardness by having heated the pure iron after performing an electroless nickel plating process on the pure iron. The base material of theiron piece 46 b and theiron core 73 b may be any soft magnetic material other than the pure iron. - A Vickers hardness of the plating of the
iron piece 46 b is greater than that of the plating of theiron core 73 b. In particularly, the Vickers hardness of the plating of theiron piece 46 b is 950 HV plus or minus 50 HV. The Vickers hardness of the plating of theiron core 73 b is 750 HV plus or minus 50 HV. Thus, the difference in the Vickers hardness between the plating of theiron piece 46 b and the plating of theiron core 73 b is 100 HV or more and 300 HV or less. Also, the Vickers hardness of the plating of theiron piece 46 b is 900 HV or more and 1000 HV or less. The Vickers hardness of the plating of theiron core 73 b is 700 HV or more and 800 HV or less. Additionally, the same configuration is applicable to the iron piece of the leading blade-drive lever 40A and the iron core of theelectromagnet 70A. - A change in the adsorption force between the
iron piece 46 b and theiron core 73 b was verified before and after an endurance test of thefocal plane shutter 1 according to the present embodiment. Specifically, the voltage which was applied to thecoil 79 b and which was needed for generating a constant adsorption force between theiron piece 46 b and theiron core 73 b was measured before and after the endurance test of thefocal plane shutter 1 according to the present embodiment. In the endurance test, the trailing blade-drive lever 40B reciprocated several times such that theiron piece 46 b abutted theiron core 73 b several times.FIG. 7A is a graph of the change in the voltage which was applied to theelectromagnet 70B and which was needed for generating a constant adsorption force between theiron piece 46 b and theiron core 73 b before and after the endurance test of thefocal plane shutter 1 according to the present embodiment. The change of the voltage applied to theelectromagnet 70B was verified by use of three samples under the same condition before and after the endurance test. - As illustrated in
FIG. 7A , the voltage which was applied to thecoil 79 b and which was needed for generating a constant adsorption force between theiron piece 46 b and theiron core 73 b was not greatly changed before and after the endurance test. This means that the adsorption force between theiron piece 46 b and theiron core 73 b was not greatly changed even in a case where a constant voltage was applied to theelectromagnet 70B before and after the endurance test. - Next, a comparative example will be described. In the comparative example, by use of a focal plane shutter equipped with an iron piece and an iron core each having a Vickers hardness of the plating of about 750 HV, the voltage which was applied to an electromagnet and which was needed for generating a constant adsorption force between the iron piece and the iron core was measured before and after the endurance test.
FIG. 7B is a graph of a change in the voltage which was applied to the electromagnet and which was needed for generating a constant adsorption force between the iron piece and the iron core before and after the endurance test of the focal plane shutter according to the comparative example. - As illustrated in
FIG. 7B , the voltage which was applied to the electromagnet and which was needed for generating a constant adsorption force after the endurance test was higher than that before the endurance test. In other words, in a case where the same voltage was applied to the electromagnet, the adsorption force generated between the iron piece and the iron core after the endurance test was lower than that before the endurance test. - The reason is considered as follows. The iron piece and the iron core in the comparative example are the same in the Vickers hardness, and the Vickers hardness of the iron piece in the comparative example is smaller than that of the
iron piece 46 b in the present embodiment. Thus, the iron piece in the comparative example is easy to be worn down. For this reason, the adsorption surface of the iron piece is attached with abrasion powder or is deformed to be uneven. Thus, an air gap is formed between the iron piece and the iron core, and the area of the absorption is reduced. Therefore, supposedly, a reduction in the spatial magnetic flux density or a reduction in the surface magnetic flux density causes a reduction in the adsorption surface. - Actually, the voltage with the same value is applied to the electromagnet in a camera. Thus, the long-term use of a camera with the focal plane shutter according to the comparative example causes a reduction in the adsorption force. This causes a reduction in the period from the time when the energization of the electromagnet is stopped to the time when the iron piece is moved away from the iron core by the biasing force of the biasing member. As a result, the timing when the blades start moving might be advanced to influence the exposure period.
- In the
focal plane shutter 1 according to the present embodiment, the adsorption force is not greatly changed before and after the endurance test. This is conceivably because it becomes difficult to wear down theiron piece 46 b due to the Vickers hardness of the plating of theiron piece 46 b which is greater than that of the plating of theiron core 73 b. Accordingly, in thefocal plane shutter 1 according to the present embodiment, a reduction in the adsorption force is suppressed even for long-term use. Therefore, even when thefocal plane shutter 1 is used for a long time, the constant exposure period can be maintained, thereby suppressing the error of the exposure period from increasing. - According to the experiment results, it is difficult to reduce the adsorption force between the
iron piece 46 b and theiron core 73 b under the condition that the difference in the Vickers hardness between the plating of theiron piece 46 b and the plating of theiron core 73 b is 100 HV or more. Also, if the manufacturing cost or the like is considered, it is preferable that the difference in the Vickers hardness between the plating of theiron piece 46 b and the plating of theiron core 73 b should be 300 HV or less. Also, it is preferable that the Vickers hardness of the plating of theiron piece 46 b should be 900 HV or more and 1000 HV or less. It is preferable that the Vickers hardness of the plating of theiron core 73 b should be 700 HV or more and 800 HV or less. - Additionally, the present invention may be applied to a self-holding electromagnet. As for the self-holding electromagnet, a permanent magnet which gives magnetic force to an iron core is fixed thereto, and the iron core can adsorb and hold an iron piece in a non-energization state. The enegization of a coil wound around the iron core generates a magnetic field around the coil so as to reduce the magnetic force of the permanent magnet.
- Therefore, the adsorption force between the iron core and the iron piece is reduced, whereby a drive lever is driven by the biasing force such that the iron piece is moved away from the iron core. Even when such a self-holding electromagnet employs the
iron piece 46 b and theiron core 73 b in the present embodiment, it is possible to ensure the constant period from the time when the energization is started to the time when theiron piece 46 b is moved away from theiron core 73 b, and it is possible to ensure the constant exposure period. - While the exemplary embodiments of the present invention have been illustrated in detail, the present invention is not limited to the above-mentioned embodiments, and other embodiments, variations and modifications may be made without departing from the scope of the present invention.
- The focal plane shutter according to the present embodiment can be employed in an optical device such as a still camera or a digital camera.
- Finally, several aspects of the present invention are summarized as follows.
- According to an aspect of the present invention, there is provided a focal plane shutter including: a board including an opening; a blade opening or closing the opening; an electromagnet including an iron core and a coil for energizing the iron core; and a drive lever holding an iron piece capable of being adsorbed to the iron core, capable of moving such that iron piece is moved into and away from the iron core, and driving the blade, wherein a plating process is performed on the iron core and the iron piece, a Vickers hardness of a plating of the iron piece is greater than that of a plating of the iron core, and a difference in the Vickers hardness between the plating of the iron piece and the plating of the iron core is 100 HV or more.
- According to another aspect of the present invention, there is provided an optical device including the above focal plane shutter.
Claims (6)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2013-060209 | 2013-03-22 | ||
| JP2013060209A JP2014186126A (en) | 2013-03-22 | 2013-03-22 | Focal plane shutter and optical device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20140286632A1 true US20140286632A1 (en) | 2014-09-25 |
| US8882370B2 US8882370B2 (en) | 2014-11-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/175,280 Expired - Fee Related US8882370B2 (en) | 2013-03-22 | 2014-02-07 | Focal plane shutter and optical device |
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| Country | Link |
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| US (1) | US8882370B2 (en) |
| JP (1) | JP2014186126A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150253646A1 (en) * | 2014-03-05 | 2015-09-10 | Seiko Precision Inc. | Focal plane shutter and optical apparatus |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2017090565A (en) | 2015-11-05 | 2017-05-25 | セイコープレシジョン株式会社 | Focal plane shutter and optical device |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5664247A (en) * | 1995-06-15 | 1997-09-02 | Nikon Corporation | Shutter brake mechanism |
| US20040213561A1 (en) * | 2003-04-22 | 2004-10-28 | Nidec Copal Corporation | Focal plane shutter |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS4626554Y1 (en) * | 1968-02-06 | 1971-09-11 | ||
| JPS5527665A (en) * | 1978-08-18 | 1980-02-27 | Matsushita Electric Ind Co Ltd | Electromagnet |
| JPS6028096Y2 (en) * | 1980-11-26 | 1985-08-26 | キヤノン株式会社 | electromagnet device |
| JP2540283Y2 (en) | 1992-09-02 | 1997-07-02 | 株式会社コパル | Iron piece support structure of electromagnet device |
| JP3635075B2 (en) | 2002-06-25 | 2005-03-30 | 日本電産コパル株式会社 | Focal plane shutter for camera |
| JP2007127715A (en) | 2005-11-01 | 2007-05-24 | Canon Inc | Camera shutter device |
| JP2007232889A (en) | 2006-02-28 | 2007-09-13 | Chinontec Kk | Lens barrel |
| JP4628387B2 (en) | 2006-03-31 | 2011-02-09 | 日本電産コパル株式会社 | Focal plane shutter for camera |
| JP2008175254A (en) | 2007-01-17 | 2008-07-31 | Seiko Epson Corp | Rotating shaft support method |
-
2013
- 2013-03-22 JP JP2013060209A patent/JP2014186126A/en active Pending
-
2014
- 2014-02-07 US US14/175,280 patent/US8882370B2/en not_active Expired - Fee Related
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5664247A (en) * | 1995-06-15 | 1997-09-02 | Nikon Corporation | Shutter brake mechanism |
| US20040213561A1 (en) * | 2003-04-22 | 2004-10-28 | Nidec Copal Corporation | Focal plane shutter |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150253646A1 (en) * | 2014-03-05 | 2015-09-10 | Seiko Precision Inc. | Focal plane shutter and optical apparatus |
| US9239511B2 (en) * | 2014-03-05 | 2016-01-19 | Seiko Precision Inc. | Focal plane shutter and optical apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| US8882370B2 (en) | 2014-11-11 |
| JP2014186126A (en) | 2014-10-02 |
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